View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20805U 90083B 23027.85576251 .00000139 00000-0 12643-3 0 9990
2 20805 82.9390 338.2807 0031992 66.0339 352.2812 13.75998896625124
| Epoch (UTC): | 27 January 2023 20:32:17 |
| Eccentricity: | 0.0031992 |
| inclination: | 82.9390° |
| perigee height: | 954 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 338.2807° |
| argument of perigee: | 66.0339° |
| revolutions per day: | 13.75998896 |
| mean anomaly at epoch: | 352.2812° |
| orbit number at epoch: | 62512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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